首页> 美国政府科技报告 >Microfog Lubricant Application System for Advanced Turbine Engine Components, Phase 2. Tasks 3, 4 and 5 Wettability and Heat Transfer of Microfog Jets Impinging on a Heated Rotating Disc, and Evaluation of Reclassifying Nozzles and a Vortex Mist Generator
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Microfog Lubricant Application System for Advanced Turbine Engine Components, Phase 2. Tasks 3, 4 and 5 Wettability and Heat Transfer of Microfog Jets Impinging on a Heated Rotating Disc, and Evaluation of Reclassifying Nozzles and a Vortex Mist Generator

机译:用于先进涡轮发动机部件的microfog润滑剂应用系统,第2阶段。任务3,4和5微流体喷射器的润湿性和传热冲击加热旋转盘,并评估重新分级喷嘴和涡流雾发生器

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The wettabilities and heat transfer rates of microfog jets (oil-mist nozzle flows) impinging on a heated rotating disc were determined under an inert atmosphere of nitrogen at temperatures ranging from 600 to 800 F. The results are discussed in relation to the various factors involved in the microfog lubricant application systems. Two novel reclassifying nozzles and a vortex mist generator were also studied. (Author)

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